133 



"1 \ \ r 



A 1 1 r — I 1 r 



X/L = 0.914 < 



J I I L 



MEASUREMENT 

 THEORY 



DISPLACEMENT 

 SURFACE 



MEASUREMENT 

 ON THE BODY 



1 I 1 1 — 1 — \ — I — r 



X/L MEASUREMENTS THEORY 

 0.755 



J I I I 



FIGURE 4. Computed and measured static pressure distributions across stern boundary layer of afterbody 1. 



FIGURE 5. Computed and measured 

 static pressure distributions 

 across near wake of afterbody 1. 



